This workflow automates the high-stakes, repetitive analysis of calculating fuel-optimal evasive maneuvers, a bottleneck that consumes analyst time and risks suboptimal fuel expenditure. The operational upside comes from extending satellite operational life—directly protecting asset value—and ensuring mission continuity by integrating maneuver planning with payload scheduling. Implementation requires integrating high-fidelity orbit propagators like Orekit or GMAT with optimizer agents, ingesting live conjunction data from SOCRATES or CARA, and enforcing strict guardrails on delta-V and pointing constraints.




